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2022 IEEE International Conference on Unmanned Systems (ICUS)最新文献

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Reliability Facility Location with Fuzzy Demand and Failure Scenarios 基于模糊需求和故障场景的可靠性设施定位
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9987243
Zhiwen Huang, Hongxu Li, Yuanfu Zhong, Qian Su, Na Lv, Yingchao Zhang
Historical war experience demonstrates that crashing critical supply facility has become an efficient tactic during wartime, so it is of great strategic significance to design an efficient and reliable emergency logistics network in face of the uncertainty at war. This paper presents a scenario-based modelling method by considering both demand uncertainty and facility failure scenarios in the mathematical model and the immune genetic algorithm (IGA) is applied to solve it. A set of numerical experiments has been conducted to verify the model and effectiveness of IGA. Finally, the sensitivity analysis results show facility failure probability has a greater impact on the final location decision, which provide model and approach for the location-allocation problem during wartime.
历史战争经验表明,破坏关键补给设施已成为战时的一种有效策略,因此,面对战争的不确定性,设计高效、可靠的应急物流网络具有重要的战略意义。在数学模型中考虑需求不确定性和设备故障情景,提出了一种基于场景的建模方法,并应用免疫遗传算法(IGA)对其进行求解。通过一组数值实验验证了IGA模型及其有效性。灵敏度分析结果表明,设施故障概率对最终选址决策有较大影响,为战时选址分配问题提供了模型和方法。
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引用次数: 0
Consensus-Based Bundle Algorithm-Based Task Allocation for Unmanned Vehicles in Dangerous Environment 基于共识束算法的危险环境下无人驾驶车辆任务分配
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9987061
Zhiyu Duan, Xiaolin Chen, Ziyuan Xie
This paper solves the distributed task allocation problem based on the danger-broadcast algorithm for unmanned vehicles with the Consensus-Based Bundle Algorithm (CBBA). By defining the dangerous region that is found by the flying unmanned vehicle, the traditional Consensus-Based Bundle Algorithm is extended with the danger broadcast, which is named as Danger-broadcast Consensus-Based Bundle Algorithm (DBCBBA). In the unknown task areas, the time discount and distance are used to describe the task's revenue function. Compared with the traditional CBBA, the proposed algorithm can be adopted to a real and complex environment, and more unmanned vehicles are saved by distributed danger-broadcast architecture. In the end, simulation experiments demonstrate the performance of the proposed algorithm for the unknown danger zone.
本文采用基于共识的束算法(Consensus-Based Bundle algorithm, CBBA)解决了基于危险广播算法的无人驾驶车辆分布式任务分配问题。通过定义飞行无人机发现的危险区域,将传统的基于共识的束算法扩展为危险广播,称为危险广播共识束算法(DBCBBA)。在未知任务区域,使用时间折扣和距离来描述任务的收益函数。与传统的CBBA算法相比,该算法可以应用于真实复杂的环境,通过分布式危险广播架构节省了更多的无人驾驶车辆。最后,通过仿真实验验证了该算法在未知危险区域下的性能。
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引用次数: 0
Aircraft Maneuver Intelligent Recognition: An End-to-end Regularized Autoencoder and SVM Approach 飞机机动智能识别:端到端正则化自编码器和支持向量机方法
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9987228
Longfei Yue, Rennong Yang, Jialiang Zuo, Y. Zhang, Xiaoru Zhao, Mengda Yan
Aircraft maneuver recognition is a key issue in unmanned aerial vehicle (UAV) intelligent air combat. Aiming at inefficiency of high-dimensional time-series maneuver data analysis and low recognition accuracy of traditional methods, an end-to-end regularized autoencoder-support vector machine (RAE-SVM) method is proposed. This method combines powerful feature extraction capability of unsupervised learning based autoencoder with superior classification performance of supervised learning based SVM. According to the change rule of maneuver data and prior expert knowledge, the maneuver recognition dataset based on time period feature data is constructed. The generalization performance of RAE network and the accuracy of the model are improved by introducing regularization. The aircraft maneuver recognition model based on RAE-SVM is constructed and verified by the maneuver recognition dataset. The simulation results show that the accuracy of model recognition is as high as 92.75%. The trained model only takes 2 milliseconds to recognize a set of maneuver data and meets the near real-time requirements. Therefore, the proposed approach in this work can quickly and accurately recognize aircraft maneuver without relying on expert experience, which has certain practical value.
飞机机动识别是无人机智能空战中的一个关键问题。针对高维时间序列机动数据分析效率低、传统方法识别精度低的问题,提出了端到端正则化自编码器-支持向量机(RAE-SVM)方法。该方法将基于无监督学习的自编码器强大的特征提取能力与基于监督学习的支持向量机优越的分类性能相结合。根据机动数据的变化规律和先验专家知识,构建了基于时间段特征数据的机动识别数据集。通过引入正则化,提高了RAE网络的泛化性能和模型的精度。构建了基于RAE-SVM的飞机机动识别模型,并用机动识别数据集进行了验证。仿真结果表明,模型识别的准确率高达92.75%。训练后的模型对一组机动数据的识别时间仅为2毫秒,满足了接近实时性的要求。因此,本文提出的方法可以在不依赖专家经验的情况下快速准确地识别飞机机动,具有一定的实用价值。
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引用次数: 0
Fully Distributed Event-Driven Formation Control Over Directed Information Topologies 有向信息拓扑的全分布式事件驱动编队控制
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9987012
Tao Xu, Xiaojian Yi, G. Wen, Z. Duan
This paper studies the formation control problem of networked second-order integrator systems from a distributed event-driven perspective, where the unknown nonlinearity is involved in the system model. An event-driven formation control scheme, which consists of a fully distributed event-driven control protocol and a fully distributed triggering function, is developed in this paper. In order to handle the nonlinear dynamics, the approximation property of the neural-network control is utilized. Adaptive gains instead of constant gains are designed in the control protocol, making the control scheme fully distributed. Using the proposed triggering mechanism, the control torque of each agent is a piecewise constant function, which is updated discontinuously and asynchronously. Moreover, the information topologies among different agents are directed and the prescribed formation configuration is time-varying. These settings are more practical, but brings some difficulties to control scheme design and theoretical analysis. It is shown that under the developed control scheme, each agent can achieve the prescribed formation configuration without causing the undesired Zeno behavior. Finally, numerical simulation is performed to confirm the validity of the main theorems.
本文从分布式事件驱动的角度研究了网络二阶积分器系统的群体控制问题,其中系统模型中涉及未知非线性。本文提出了一种由全分布式事件驱动控制协议和全分布式触发功能组成的事件驱动编队控制方案。为了处理非线性动力学,利用了神经网络控制的逼近特性。在控制协议中设计了自适应增益代替恒定增益,使控制方案完全分布式。利用所提出的触发机制,每个agent的控制力矩是一个分段常数函数,该函数是不连续和异步更新的。此外,不同agent之间的信息拓扑是定向的,规定的编队配置是时变的。这些设置比较实用,但也给控制方案设计和理论分析带来了一定的困难。结果表明,在所设计的控制方案下,各agent均能达到规定的编队配置,而不会产生不期望的芝诺行为。最后,通过数值仿真验证了主要定理的有效性。
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引用次数: 0
CST-GANs: A Generative Adversarial Network Based on CST Parameterization for the Generation of Smooth Airfoils CST- gan:基于CST参数化的光滑翼型生成对抗网络
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9987080
Jinxing Lin, Chenliang Zhang, Xiaoye Xie, Xingyu Shi, Xiaoyu Xu, Yanhui Duan
Generative adversarial networks (GANs) are well-known for their powerful generation ability. In recent years, GANs have been applied in the field of aerodynamic shape optimization (ASO). However, the existing airfoil generation methods based on GANs can only generate a discrete sequence of coordinates corresponding to fixed abscissas, and cannot be applied to the scenarios that generate airfoils directly. In this paper, class function / shape function transformation (CST), a parameterization method of the airfoil that forms a good representation of the geometric shape of the airfoil, is combined with GANs. Therefore, a CST-GANs method is proposed that can directly generate the CST parameterized variables of the airfoil instead of a sequence of airfoil points. Given the abscissa and parameterized variables, the corresponding coordinate can be calculated by CST expression. On the other hand, CST-GANs can generate airfoil geometry with smooth surface without intro-ducing the Bézier curve or the Savitzky-Golay filter. Experiments show that CST-GANs is a promising model, which can not only generate smoother airfoils with fewer neural network parameters but also generate more diverse airfoils.
生成对抗网络(GANs)以其强大的生成能力而闻名。近年来,gan已被应用于气动形状优化(ASO)领域。然而,现有的基于gan的翼型生成方法只能生成与固定横坐标对应的离散坐标序列,不能应用于直接生成翼型的场景。本文将类函数/形状函数变换(class function / shape function transformation, CST)这一能够很好地表征翼型几何形状的参数化方法与gan相结合。因此,提出了一种CST- gans方法,该方法可以直接生成翼型的CST参数化变量,而不是翼型点序列。给定横坐标和参数化变量,可以通过CST表达式计算相应的坐标。另一方面,cst - gan可以产生表面光滑的翼型几何形状,而无需引入bsamizier曲线或Savitzky-Golay滤波器。实验表明,cst - gan模型不仅可以用更少的神经网络参数生成更光滑的翼型,而且可以生成更多样化的翼型,是一种很有前途的模型。
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引用次数: 2
Track Matching Method of Sea Surface Targets Based on Improved Longest Common Subsequence Algorithm 基于改进最长公共子序列算法的海面目标航迹匹配方法
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9986530
Dewei Deng, Ziqian Xiong, Chuan Wang, Hao Liu
Track similarity analysis is an important part of historical track big data mining analysis, which provides a basis for track clustering, target recognition, and target activity law analysis. The paper adopts the improved longest common subsequence method to measure the similarity between different tracks and complete track matching. Firstly, we establish a historical track database and establish a raster spatial index for the key sea areas of concern. Secondly, we preprocess the track data and unify the data of different sampling scales into one space-time dimension through sparse or interpolation, retrieve historical tracks that are geographically close to the current track, and use the improved longest common subsequence method to calculate the matching similarity probability between the current track and the historical track. Finally, the track clustering and activity rule mining analysis are completed according to the calculated maximum matching probability. The simulation experiment verifies that the algorithm can effectively calculate and complete the correlation matching of target tracks, which provides an effective basis for target track clustering and activity law mining and analysis.
航迹相似度分析是历史航迹大数据挖掘分析的重要组成部分,为航迹聚类、目标识别和目标活动规律分析提供了基础。本文采用改进的最长公共子序列法测量不同航迹之间的相似度,实现航迹的完全匹配。首先,建立历史航迹数据库,建立重点关注海域的栅格空间指数;其次,对航迹数据进行预处理,通过稀疏或插值将不同采样尺度的数据统一到一个时空维度,检索地理上与当前航迹接近的历史航迹,并使用改进的最长公共子序列法计算当前航迹与历史航迹的匹配相似概率;最后,根据计算出的最大匹配概率完成航迹聚类和活动规则挖掘分析。仿真实验验证了该算法能够有效地计算并完成目标航迹的相关匹配,为目标航迹聚类和活动规律挖掘分析提供了有效依据。
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引用次数: 0
A Light Field Image Quality Assessment Method Based on Stereo Vision 基于立体视觉的光场图像质量评价方法
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9986647
Wei Fu, Xingfa Shen, Wenhui Zhou, A. Zhdanov, Chuntong Geng
Light field imaging is an important achievement in visual information exploration in recent years, which can capture more abundant visual information from the real world. However, most existing light field image quality assessment (LF-IQA) indicators rely heavily on feature extraction based on high complexity statistics in quality evaluation tasks, which is not comprehensive in future modern applications or power-limited devices. To solve this problem, the research puts forward a light field image quality evaluation method based on stereo vision. By introducing a brand-new light field image coding method and training the neural network, the purpose of image quality evaluation is finally achieved. Some experiments show that our model achieves good results in open source data sets.
光场成像是近年来视觉信息探索领域的一项重要成果,它可以从现实世界中获取更丰富的视觉信息。然而,现有的光场图像质量评估(LF-IQA)指标在质量评估任务中大多依赖于基于高复杂度统计的特征提取,在未来的现代应用或功率有限的设备中,这种方法并不全面。针对这一问题,研究提出了一种基于立体视觉的光场图像质量评价方法。通过引入一种全新的光场图像编码方法并对神经网络进行训练,最终达到图像质量评价的目的。实验表明,该模型在开源数据集上取得了较好的效果。
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引用次数: 0
Real-time Guidance for Powered Landing of Reusable Rockets via Deep Reinforcement Learning 基于深度强化学习的可重复使用火箭动力着陆实时制导
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9986540
Linfeng Su, Jinbo Wang, Zhenwei Ma, Hongbo Chen
Powered landing of reusable rocket is an advanced technology to achieve pinpoint landing (the norm of position error < 5 m and velocity error < 2 m/s) while satisfying a series of highly nonlinear constraints. A major challenge is guaranteeing fuel-optimal and convergence when solving rocket powered landing problem. In this manuscript, a real-time feedback guidance algorithm based on deep reinforcement learning is developed. The proposed method maps state directly to thrust control commands. The first contribution of this paper is to use multi-stage reward function to eliminate the negative effects triggered by design guidance law, thereby significantly enhancing fuel-optimal performance. Another contribution is that a model pre-training framework based on imitation learning is presented to improve model convergence by fitting optimal data. Numerical experiments show that the nearly fuel-optimal trajectories generated by the proposed algorithm successfully achieve pinpoint landing from random initial states.
可重复使用火箭动力着陆是在满足一系列高度非线性约束条件下实现精确着陆(位置误差小于5 m、速度误差小于2 m/s)的先进技术。在解决火箭动力着陆问题时,如何保证燃料的最优性和收敛性是一个重要的挑战。本文提出了一种基于深度强化学习的实时反馈制导算法。所提出的方法将状态直接映射到推力控制命令。本文的第一个贡献是利用多级奖励函数消除了设计制导律引发的负面影响,从而显著提高了燃油最优性能。另一个贡献是提出了一个基于模仿学习的模型预训练框架,通过拟合最优数据来提高模型的收敛性。数值实验表明,该算法生成的近燃料最优轨迹成功地从随机初始状态实现了精确着陆。
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引用次数: 1
An Object Detection Algorithm for Military Vehicles Based on Image Style Transfer and Domain Adversarial Learning 基于图像风格转移和领域对抗学习的军用车辆目标检测算法
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9987190
Yubeibei Zhou, Jiulu Gong, Weijian Lu, Naiwei Gu, Kuiqi Chong, Zepeng Wang
In order to improve the accuracy of object detection based on deep learning for military vehicles., an object detection algorithm based on image style transfer and domain adversarial learning is proposed. Aiming at the problem of the small number of military vehicle images., a military vehicle image dataset is constructed by using games., miniature models and spider technology. However., due to the visual difference between these images., the accuracy of the trained detection model is poor when it is directly used to detect the actual collected images. CycleGAN is used for image style transfer to obtain images with a similar style to military vehicle images at the data level. Domain adversarial learning is used to optimize the one-stage object detection algorithm to make the network learn domain invariant features and reduce the domain discrepancy at the feature level. The proposed algorithm is implemented with YOLOv5s as an example. The test results show that the proposed algorithm improves the average precision (AP) by 5.7% without increasing the amount of inference computation., compared with the YOLOv5s algorithm.
为了提高基于深度学习的军用车辆目标检测精度。提出了一种基于图像风格迁移和领域对抗学习的目标检测算法。针对军用车辆图像数量少的问题。,利用游戏方法构建了军用车辆图像数据集。微型模型和蜘蛛技术。然而。由于这些图像之间的视觉差异。,训练后的检测模型直接用于检测实际采集的图像时,准确率较差。CycleGAN用于图像样式转移,在数据级获得与军用车辆图像样式相似的图像。利用领域对抗学习对单阶段目标检测算法进行优化,使网络能够学习到领域不变的特征,并在特征层次上减少领域差异。该算法以YOLOv5s为例进行了实现。测试结果表明,该算法在不增加推理计算量的情况下,平均精度提高了5.7%。,与YOLOv5s算法相比。
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引用次数: 1
Customized First Order Convex Optimization Algorithm for Powered-Descent Guidance 自定义一阶凸优化算法的动力下降制导
Pub Date : 2022-10-28 DOI: 10.1109/ICUS55513.2022.9986982
Jiarui Ma, Jinbo Wang, Qiliang Zhang
This paper introduces the extrapolated proportional integral projected gradient (ePIPG) method, a newly developed first-order method, for second-order cone programming problems (SOCP), and its customized implementation to solve the 3-DoF powered-descent guidence problem. The ePIPG solvers parse the problem parametets automatically to fully utilize the problem sparse structure. In addition, different from the classic interior-point method, being a first-order method, ePIPG only relies on simple algebra operations, for example, projection onto convex sets, multiplication of matrix and vector and vectors addition. The numerical experiment shows that the customized ePIPG solver is significantly faster than ECOS and GUROBI, two advanced convex optimization solvers, thus is a potential method for future rocket landing missions.
介绍了一种求解二阶锥规划问题(SOCP)的一阶新方法——外推比例积分投影梯度法(ePIPG),并给出了该方法在求解三自由度动力下降制导问题中的具体实现。ePIPG求解器自动解析问题参数,充分利用问题的稀疏结构。此外,与经典的内点法不同,ePIPG是一阶方法,它只依赖于简单的代数运算,如凸集上的投影、矩阵与向量的乘法、向量的加法。数值实验表明,自定义ePIPG求解器的求解速度明显快于ECOS和GUROBI两种先进的凸优化求解器,是未来火箭着陆任务的一种有潜力的方法。
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引用次数: 0
期刊
2022 IEEE International Conference on Unmanned Systems (ICUS)
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